US3080748A - Strain detection apparatus - Google Patents

Strain detection apparatus Download PDF

Info

Publication number
US3080748A
US3080748A US855667A US85566759A US3080748A US 3080748 A US3080748 A US 3080748A US 855667 A US855667 A US 855667A US 85566759 A US85566759 A US 85566759A US 3080748 A US3080748 A US 3080748A
Authority
US
United States
Prior art keywords
electro
plastic body
conductive
plastic
frangible
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US855667A
Inventor
Ralph A Burkley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Goodyear Aircraft Corp
Original Assignee
Goodyear Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Goodyear Aircraft Corp filed Critical Goodyear Aircraft Corp
Priority to US855667A priority Critical patent/US3080748A/en
Application granted granted Critical
Publication of US3080748A publication Critical patent/US3080748A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0033Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/16Measuring arrangements characterised by the use of electric or magnetic techniques for measuring the deformation in a solid, e.g. by resistance strain gauge
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0025Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings of elongated objects, e.g. pipes, masts, towers or railways
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0083Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by measuring variation of impedance, e.g. resistance, capacitance, induction

Definitions

  • This invention relates to strain detection apparatus, and more particularly, is concerned with apparatus for the detection of strains in articles of various materials such as reinforced plastics and the like, the apparatus normally functioning without the destruction of the article subjected to strains.
  • non-destructive testing methods have been utilized in testing the strength and fatigue characteristics of plastic structures, and particularly reinforced plastic structures.
  • Such non-destructive testing methods included ing transmitted light, ultrasonic testing, and static load testing, are not fully satisfactory, and there has been a need for testing procedures offering more specific information and increased reliability.
  • Another object of the invention is the provision of apparatus of the type described utilizing a single or a multiplicity of metallic or metallic coated filaments so connected in electric circuits and built into the plastic structure whereby strains imparted to the structure break the electrical continuity of at least certain of the filaments to provide an electrical indication of the strains imparted to the plastic structure.
  • the foregoing objects of the invention, and other objects which will become apparent as the description proceeds, are achieved by the provision of a single or plurality of frangible electric conductors positioned in substantially parallel relation to each other and adapted to be an integral part of a reinforced plastic structure so as to be strained when the structure is strained, an electric lead to each conductor, and means for determining whether and which electric conductors have been broken when the structure is strained.
  • the gauge apparatus may include a galvanometer, a source of electric current,
  • FIG. 1 is a diagrammatic plan view of a strain detection apparatus, partially broken away, incorporating the principles of the invention
  • FIG. 2 is a fragmentary cross-sectional view of the apparatus taken on line 2-2 of FIG. 1;
  • FIGS. 3, 4, 5, and 6 illustrate cross-sectional views, on enlarged scale, through three different electro-condu'ctive filaments constructed in accord with the invention
  • FIG. 7 is a view on a reduced scale of the strain gauge wafer forming a part of the apparatus of FIG. 1;
  • FIG. 8 is a view similar to FIG. 7 but of a modification of the form of the invention shown in FIG. 7;
  • FIG. 9 is a view similar to FIG. 2 but of a modification of the form of the invention shown in FIG. 2;
  • FIG. ll is a cross-sectional exaggerated view similar to FIGS. 2 and 9 but of still another form of the invention and using but a single frangible electric conductor;
  • FIG. 11 is a diagrammatic exaggerated view of a typical filament-wound article utilizing the strain detection element of the invention.
  • FIG. 12 is a diagrammatic view of another filamentwound article showing another embodiment of the strain detection element of the invention.
  • the numeral 1 indicates a flat flexible sheet of non-conductive material such as plastic or similar material having electrical insulating characteristics, and positioned on this sheet are a plurality of frangible electrical conductors 2, usually arranged in substantially parallel relationship in the manner illustrated.
  • Each electrical conductor 2 is secured at one end to a connector member 3, such as a strip of metal or foil or conductive paint and at its other end is connected to a single conductive connector plate 4, the several plates being spaced along the edge of the sheet 1 opposite to the connector member 3.
  • FIG. 1 Covering the electrical conductors 2, the connector member 3 and connector plates 4 is a second flexible sheet of insulating material 5 which is compacted down against all of the parts of the sheet 1 to form a flat flexible wafer or sandwich gauge member indicated as a whole by the numeral 6 and shown partially in cross section in FIG. 2. It will be recognized that in FIG. 1 the covering sheet 5 has been broken away from the upper half of the water 6 to better illustrate the construction thereof.
  • strain member or wafer 6 Associated with the strain member or wafer 6 is apparatus indicated as a whole by the numeral 7 and including a galvanorneter 8, a multi-point switch 9 and a source of electric current 12, these three elements being electrically connected in series in the manner illustrated.
  • Each of the points of the multi-point switch 9 has an electric resistance 19 connected thereto, the resistances 10 being of progressively increased value in the manner shown by their progressively increasing length, and with the end of each resistance 10 remote from the switch -9 being connected by a flexible electric lead 11 to one of the single connector plates 4 in the manner shown.
  • the connector member 3 is connected by a flexible wire 11a to the source of electric current 12.
  • FIG. 3 illustrates one manner of constructing the frangible electric conductor 2, this embodiment of the invention including an electro-conductive core 13 having an insulating cover 14.
  • FIG. 4 shows another manner of constructing the conductor 2 by providing an insulating core 15', an electro-conductive layer 16 surrounding the core 15, and a covering layer 17 of insulating material.
  • FIG. 5 shows still another manner of constructing the electrical conductor 2 by using a core '18 of electro-conductive material, a covering layer 19 of insulating material, a cover or-layer -20 of eleotro-conductive -material, and a final covering layer 21 of insulating material.
  • FIG. 6 is a cross-section of another form of the conductor 2utilizinga construction similar'to that of FIG. '5 but with an insulating core 22, an electro-conductive layer 23 surrounding the core 22, an insulatingcovering layer 24 over the conductive layer 23, -a second electroconductive layer 25 over the insulating'layer 24, 'anda second insulating layer 26 overthe conductive layer 25.
  • FIGS. and '6 are especially useful in certain applications where'the element is'woundin continuous integral form and it is desired to not only ascertain whether electrical continuity has been interrupted, but also at what .pointin the structure.
  • the non-conductive core '15 may be similarly of any suitable material, for example,'a single filament of glass quartz, alumina, plastics, and the like, or a roving strand consisting of a multiple number of single similar filaments with the entire strand being conductively coated by means well-known in the art suchas'passage through a molten bath or vacuum deposition techniques.
  • Tensile elongations of the electrical conductors 2 before breaking of the electrical conductive characteristic may be made to fall within the ranges of elongation to which the structure to be tested is subjected. Usually these ranges for strain determinations in structures extend from about 0.001 to about 4.0 percent elongation. it will be recognized that elongationpercent-ages even as high as 100% can'be achieved by appropriate selection of suitable specific materials having the desired dimen- 'sional characteristics and to provide loss of electrical conductivity when elongated to thepercentages stated.
  • the strain detection apparatus of the invention takes three'basic forms. The first is that illustrated in FIG. 1 wherein'each electrical conductor 2 when progressing from one side to the other of the wafer'& has a progressively higher strain level before it becomes electrically nonconductive through its adjacent conductor.
  • the conductor 2 shown at-the top of FIG. 1 is constructed to become electrically non-conductive when subjected to an elongation of 05 percent, the next lower conductor-2 at 1.0 percent, thenext lo'we'r conductor 2 at 1.5 percent, and'so on, down-across the wafrd.
  • the conductors '2 can be placed relatively closely together, and the output of the wafer6'wlren connected to the indicating means 7 indicates within'one-half of one percent "the tensile elongation.
  • FIG. 8 The second basic form of the invention is shown in FIG. 8 wherein the wafer 27 is formed of conductors 2 all having substantially 'the same elongation in tensile strain direction before becoming electrically non conductive.
  • the conductors 2 are normally positioned farther apart, with the wafer-27 being of larger size.
  • a wafer of this type when built into a structure to be tested will indicate when safe limits are exceeded, for example, in any part of the structure covered by the wafer 27.
  • Indicating means 7 can be used with wafer 27 with or without resistances to show which frangible conductors have been broken.
  • FIG. 1 The thirdbasic form of the invention is shown in FIG. 1
  • frangible electrical conductor 31 is wound in simultaneously-with load carrying strands 32, for example as' a tape 3-3, to reinforce a plastic structure 34.
  • the conductor 31 and strands 32 may, for example, be wound helically with conductor 31 periodically reappearing in a sectional view like FIG. 10.
  • the conductor is wound entirely through the plastic structure whether it be tube, nozzle, rocket casing, nose cone, or some other article, and with some portion of the conductor being broken and rendered electrically nonconductive ifthe plastic structure cracks or is otherwise st-rained or broken beyond accept-able limits.
  • a goor no go indicator is thusbuilt into a pla'stic structure which can'be' quickly checked atany time duringthe life or use of the structure.
  • FIG. 11 shows such use with a typical'fila'ment wound article 35.
  • such articles are formed by the helical Winding von a rotating-mandrel of continuous lengths of resin-impregnated filaments; such structure subsequently'being cured to provide a finished piece.
  • the filament-wound article has incorporated throughout its structure at least one conductive length, the two ends of which are brought out to testing terminals 37 for use with associated'equipment as described hereinbefore in connection with FIG. -1.
  • FIG. 12 another form of utilizing conductive elements 38 in conjunction with a filament-wound article 39 is shown.
  • Such elements 38 are wound sinuousoidally in a circumferential manner either 'onthe surface of'the article 39 or preferably laid intothe wall itself, with testing terminals 40 provided at the ends of the element 38,
  • any of the filament or strand element constructions shown in FIGS. 3, '4, 5, 01'6 can be utilized as the elements in FIGS. 11 and 12, and that such elements can be used in the combination forms shown in FIGS. 2, 9 and 10.
  • Indicating rneans such as means '7, will be used with the forms of the invention heretobefore described.
  • such strain wafers can-be constructed into a plastic structure in any desired layer or direction, and particularly in critical structural areas, and with the electrical conductors of the strain wafers normally extending in the same direction as the reinforcing means for the plastic structure.
  • utilizing the'different and progressively increasing resistors '10 means that the galvanometer 8 can be calibrated in terms of percent of strain and will so'register when themultipoint switch 9 is'swun'g from leftto right until the first unbroken electrical conductor 2 is reached. 'Ifthere sistors 10 are eliminated the galvanometerdshows which conductors 2 are broken.
  • a hollow plastic body flexible, body-reinforcing load-carrying strands embedded in-and extending helically as a continuous tape through the plastic body and molded integrally therewith, flexible, frangible, electro-conductive strand means forming a part of the'tape and extending parallel to and coextensive with the load-carrying strands and molded integrally into the sesame plastic body therewith, electric leads extending from the ends of said electro-conductive strand means out of the plastic body, and electrical means adapted to be connected to said leads for determining if t e electro-conductive strand means are unbroken to thereby determine the soundness of the plastic body after the making or use thereof, said frangible, electro-conductive strand means being of a strength which will break if the safe limits of stress imposed upon the plastic body are exceeded.
  • a hollow plastic body flexible, body-reinforcing load-carrying strands embedded in and extending helically as a continuous tape through the plastic body and molded integrally therewith, fiexibie, frangible, electro-conductive strand means forming a part of the tape and extending parallel to and coextensive with the load-carrying strands and molded integrally into the plastic body therewith, and electric leads extending from the ends of said electro-conductive strand means out of the plastic body, said frangible, electro-conductive strand means being of a strength which will break in the safe limits of stress imposed upon the plastic body are exceeded.
  • a hollow plastic body flexible, body-reinforcing load-carrying strands embedded in and extending continuously through the plastic body and molded integrally therewith, flexible, frangible, electroconductive strand means forming a part of the load-carrying strands and extending parallel to and coextensive with the load-carrying strands and molded integrally into the plastic body therewith, and electric leads extending from the ends of said electro-conductive strand means out of 6 the plastic body, said frangible, electro-conductive strand means being of a strength which will break if the plastic body is cracked.
  • a reinforced plastic member including a hard, cured plastic body made rom a tape wound over itself to form the body, the tape havin a plurality of plastic-impregnated, flexible, load-carrying strands extending longitudinally of the tape and parallel to each other, and the tape having a single electro-conductive, plastic-impregnated, flexible but frangible strand means extending longitudinally of the tape and parallel to ti e load-carrying strands so as to be Wound entirely through the plastic body, and electric leads connected to the ends of the electro-conductive strand means and extending outside the body whereby the electrical continuity of the electro-conductive strand means can be tested at any time after the curing of the body to thereby provide a checx on the continuity of the body.
  • electro-conductive strand means have an electrically nonconductive core means surrounded by an electro-conducti /e surface layer.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)

Description

March 12, 1963 R. A. BURKLEY 3,080,748
STRAIN DETECTION APPARATUS Filed Nov. 27, 1959 2 Sheets-Sheet 1 FlG.-7
32 FlG.lO 32 ATTORNEY ll lll ll lli llll IL llllLllllfllllnlLlllLlvll FlG.-8
March 12, 1963 R. A. BURKLEY STRAIN DETECTION APPARATUS 2 Sheets-Sheet 2 Fl.ll
Filed NOY. 27, 1959 INVENTOR. RALPH A. BURKLEY BY WM ATTORNEY 343%,748 STRAEN DETEKITHGN APRARATUS Ralph A. Barkley, Cuyahcga Falls, (this, assignor to Goodyear Aircraft Corporation, Akron, Ohio, a corpc ration of Delaware Filed Nov. 27, 1959, Ser. No. 855,667 Claims. (Cl. 73--88.5)
This invention relates to strain detection apparatus, and more particularly, is concerned with apparatus for the detection of strains in articles of various materials such as reinforced plastics and the like, the apparatus normally functioning without the destruction of the article subjected to strains.
Heretofore, non-destructive testing methods have been utilized in testing the strength and fatigue characteristics of plastic structures, and particularly reinforced plastic structures. Such non-destructive testing methods, includ ing transmitted light, ultrasonic testing, and static load testing, are not fully satisfactory, and there has been a need for testing procedures offering more specific information and increased reliability.
Conventional electrical resistance strain gauges do not particularly adapt themselves to fabrication into rei11- forced plastic structures and improved non-destructive test methods have been found desirable to ascertain the structural integrity of a plastic part on the basis of the absence of cracks, flaws, structural imperfections and residual stress concentrations in critical areas.
It is the general object of the present invention to avoid and overcome the foregoing and other difiiculties of and objections to prior art practices by the provision of an improved relatively inexpensive strain detection apparatus capable of being built into or attached to a plastic structure, and particularly a reinforced plastic structure, to accurately detect the location and magnitude of critical stresses therein.
Another object of the invention is the provision of apparatus of the type described utilizing a single or a multiplicity of metallic or metallic coated filaments so connected in electric circuits and built into the plastic structure whereby strains imparted to the structure break the electrical continuity of at least certain of the filaments to provide an electrical indication of the strains imparted to the plastic structure.
Another object of the invention is to provide a strain gauge wherein frangible filament type materials of progressively breakable type are selected to cover the range of strain limits required in a given application, the apparatus being adapted to all phases of fabrication and qualification testing, the inspection or" parts in storage and at any other time in the operational life of the part.
Another object of the invention is to provide in combination a plastic structure reinforced with strands, filaments, cords, or the like with at least one of such members being a frangible electric conductor running entirely through the plastic structure over substantially all areas thereof and whereby a test at any time of the electrical continuity of the conductor indicates any failure of the plastic structure.
The foregoing objects of the invention, and other objects which will become apparent as the description proceeds, are achieved by the provision of a single or plurality of frangible electric conductors positioned in substantially parallel relation to each other and adapted to be an integral part of a reinforced plastic structure so as to be strained when the structure is strained, an electric lead to each conductor, and means for determining whether and which electric conductors have been broken when the structure is strained. The gauge apparatus may include a galvanometer, a source of electric current,
3,980,748 Patented Mar. 12, 1963 2 and a multi-point switch, for example, to facilitate determination of whether and which frangible conductors are broken when the plastic part being tested is strained.
For a better understanding of the invention reference should be had to the accompanying drawings wherein FIG. 1 is a diagrammatic plan view of a strain detection apparatus, partially broken away, incorporating the principles of the invention;
FIG. 2 is a fragmentary cross-sectional view of the apparatus taken on line 2-2 of FIG. 1;
FIGS. 3, 4, 5, and 6 illustrate cross-sectional views, on enlarged scale, through three different electro-condu'ctive filaments constructed in accord with the invention;
FIG. 7 is a view on a reduced scale of the strain gauge wafer forming a part of the apparatus of FIG. 1;
FIG. 8 is a view similar to FIG. 7 but of a modification of the form of the invention shown in FIG. 7;
FIG. 9 is a view similar to FIG. 2 but of a modification of the form of the invention shown in FIG. 2;
FIG. ll) is a cross-sectional exaggerated view similar to FIGS. 2 and 9 but of still another form of the invention and using but a single frangible electric conductor;
FIG. 11 is a diagrammatic exaggerated view of a typical filament-wound article utilizing the strain detection element of the invention; and
FIG. 12 is a diagrammatic view of another filamentwound article showing another embodiment of the strain detection element of the invention.
In the drawings, the numeral 1 indicates a flat flexible sheet of non-conductive material such as plastic or similar material having electrical insulating characteristics, and positioned on this sheet are a plurality of frangible electrical conductors 2, usually arranged in substantially parallel relationship in the manner illustrated. Each electrical conductor 2 is secured at one end to a connector member 3, such as a strip of metal or foil or conductive paint and at its other end is connected to a single conductive connector plate 4, the several plates being spaced along the edge of the sheet 1 opposite to the connector member 3. Covering the electrical conductors 2, the connector member 3 and connector plates 4 is a second flexible sheet of insulating material 5 which is compacted down against all of the parts of the sheet 1 to form a flat flexible wafer or sandwich gauge member indicated as a whole by the numeral 6 and shown partially in cross section in FIG. 2. It will be recognized that in FIG. 1 the covering sheet 5 has been broken away from the upper half of the water 6 to better illustrate the construction thereof.
Associated with the strain member or wafer 6 is apparatus indicated as a whole by the numeral 7 and including a galvanorneter 8, a multi-point switch 9 and a source of electric current 12, these three elements being electrically connected in series in the manner illustrated. Each of the points of the multi-point switch 9 has an electric resistance 19 connected thereto, the resistances 10 being of progressively increased value in the manner shown by their progressively increasing length, and with the end of each resistance 10 remote from the switch -9 being connected by a flexible electric lead 11 to one of the single connector plates 4 in the manner shown. The connector member 3 is connected by a flexible wire 11a to the source of electric current 12.
PKG. 3 illustrates one manner of constructing the frangible electric conductor 2, this embodiment of the invention including an electro-conductive core 13 having an insulating cover 14. FIG. 4 shows another manner of constructing the conductor 2 by providing an insulating core 15', an electro-conductive layer 16 surrounding the core 15, and a covering layer 17 of insulating material. FIG. 5 shows still another manner of constructing the electrical conductor 2 by using a core '18 of electro-conductive material, a covering layer 19 of insulating material, a cover or-layer -20 of eleotro-conductive -material, and a final covering layer 21 of insulating material.
FIG. 6 is a cross-section of another form of the conductor 2utilizinga construction similar'to that of FIG. '5 but with an insulating core 22, an electro-conductive layer 23 surrounding the core 22, an insulatingcovering layer 24 over the conductive layer 23, -a second electroconductive layer 25 over the insulating'layer 24, 'anda second insulating layer 26 overthe conductive layer 25.
The forms ofelement shown in FIGS. and '6 are especially useful in certain applications where'the element is'woundin continuous integral form and it is desired to not only ascertain whether electrical continuity has been interrupted, but also at what .pointin the structure.
It will be understood'that various materials can be utilized forthe electrical conductors 2, with the materials being adapted to be'electrica-lly broken when subjected to specific tensile elongations. Many materials may be utilized as a-con-ducting media-and in'the class of metals utilized in the conductor structure of FIG. 3, for example, aluminum, steel, titanium, or the'like, are-applicable. 'In electrical conductors of the type shownin FIG. 4, the non-conductive core '15 may be similarly of any suitable material, for example,'a single filament of glass quartz, alumina, plastics, and the like, or a roving strand consisting of a multiple number of single similar filaments with the entire strand being conductively coated by means well-known in the art suchas'passage through a molten bath or vacuum deposition techniques.
Tensile elongations of the electrical conductors 2 before breaking of the electrical conductive characteristic may be made to fall within the ranges of elongation to which the structure to be tested is subjected. Usually these ranges for strain determinations in structures extend from about 0.001 to about 4.0 percent elongation. it will be recognized that elongationpercent-ages even as high as 100% can'be achieved by appropriate selection of suitable specific materials having the desired dimen- 'sional characteristics and to provide loss of electrical conductivity when elongated to thepercentages stated.
The strain detection apparatus of the invention takes three'basic forms. The first is that illustrated in FIG. 1 wherein'each electrical conductor 2 when progressing from one side to the other of the wafer'& has a progressively higher strain level before it becomes electrically nonconductive through its adjacent conductor. For example, the conductor 2 shown at-the top of FIG. 1 is constructed to become electrically non-conductive when subjected to an elongation of 05 percent, the next lower conductor-2 at 1.0 percent, thenext lo'we'r conductor 2 at 1.5 percent, and'so on, down-across the wafrd. In this type wafer, 'asshown in both "FIGS. 1 and 7, the conductors '2 can be placed relatively closely together, and the output of the wafer6'wlren connected to the indicating means 7 indicates within'one-half of one percent "the tensile elongation.
The second basic form of the invention is shown in FIG. 8 wherein the wafer 27 is formed of conductors 2 all having substantially 'the same elongation in tensile strain direction before becoming electrically non conductive. In this form of the invention the conductors 2 are normally positioned farther apart, with the wafer-27 being of larger size. A wafer of this type when built into a structure to be tested will indicate when safe limits are exceeded, for example, in any part of the structure covered by the wafer 27. Indicating means 7 can be used with wafer 27 with or without resistances to show which frangible conductors have been broken.
9 illustrates "a modification of 'the invention wherein-frangible electric conductors 28 of the same type asthe conductors 2 can be directly secured, as by cement -29 directlyto aplastic structure 30 which is adapted to be tested.
The thirdbasic form of the invention is shown in FIG.
10, wherein only a single frangible electrical conductor 31 is wound in simultaneously-with load carrying strands 32, for example as' a tape 3-3, to reinforce a plastic structure 34. The conductor 31 and strands 32 may, for example, be wound helically with conductor 31 periodically reappearing in a sectional view like FIG. 10. In this man nor, the conductor is wound entirely through the plastic structure whether it be tube, nozzle, rocket casing, nose cone, or some other article, and with some portion of the conductor being broken and rendered electrically nonconductive ifthe plastic structure cracks or is otherwise st-rained or broken beyond accept-able limits. A goor no go indicator is thusbuilt into a pla'stic structure which can'be' quickly checked atany time duringthe life or use of the structure.
FIG. 11 shows such use with a typical'fila'ment wound article 35. As is well known in the art, such articles are formed by the helical Winding von a rotating-mandrel of continuous lengths of resin-impregnated filaments; such structure subsequently'being cured to provide a finished piece. Thus utilizing the construction of FIG. 10, for example, as element 36 of FIG.'1l, the filament-wound article has incorporated throughout its structure at least one conductive length, the two ends of which are brought out to testing terminals 37 for use with associated'equipment as described hereinbefore in connection with FIG. -1. It will be obvious that although the element fao as shown only traverses the length of the article 35 once, it is preferred in actual practice tohave theelement 36interwoven in the same manner as an adjacent reinforcing element-such as 32 of FIG. 10 throughout the entire structure.
In FIG. 12 another form of utilizing conductive elements 38 in conjunction with a filament-wound article 39 is shown. Such elements 38 are wound sinuousoidally in a circumferential manner either 'onthe surface of'the article 39 or preferably laid intothe wall itself, with testing terminals 40 provided at the ends of the element 38,
It will be understood that any of the filament or strand element constructions shown in FIGS. 3, '4, 5, 01'6 can be utilized as the elements in FIGS. 11 and 12, and that such elements can be used in the combination forms shown in FIGS. 2, 9 and 10.
Indicating rneans, such as means '7, will be used with the forms of the invention heretobefore described.
Furthermore, in the use of the apparatus of the invention shown in FIG. 7 or 8, such strain wafers can-be constructed into a plastic structure in any desired layer or direction, and particularly in critical structural areas, and with the electrical conductors of the strain wafers normally extending in the same direction as the reinforcing means for the plastic structure.
In the-form of the invention shown in FIG. '1, utilizing the'different and progressively increasing resistors '10 means that the galvanometer 8 can be calibrated in terms of percent of strain and will so'register when themultipoint switch 9 is'swun'g from leftto right until the first unbroken electrical conductor 2 is reached. 'Ifthere sistors 10 are eliminated the galvanometerdshows which conductors 2 are broken.
While a certain representative embodiment. and details have been shown for the purpose of illustrating "the invention, it will be apparent tothose'skilled'inthis arttha't various changes and modifications maybe made therein without departin'g from the spirit or scope ofthe in vention.
What is claimed'is:
1. In combination, a hollow plastic body, flexible, body-reinforcing load-carrying strands embedded in-and extending helically as a continuous tape through the plastic body and molded integrally therewith, flexible, frangible, electro-conductive strand means forming a part of the'tape and extending parallel to and coextensive with the load-carrying strands and molded integrally into the sesame plastic body therewith, electric leads extending from the ends of said electro-conductive strand means out of the plastic body, and electrical means adapted to be connected to said leads for determining if t e electro-conductive strand means are unbroken to thereby determine the soundness of the plastic body after the making or use thereof, said frangible, electro-conductive strand means being of a strength which will break if the safe limits of stress imposed upon the plastic body are exceeded.
2. In combination, a hollow plastic body, flexible, body-reinforcing load-carrying strands embedded in and extending helically as a continuous tape through the plastic body and molded integrally therewith, fiexibie, frangible, electro-conductive strand means forming a part of the tape and extending parallel to and coextensive with the load-carrying strands and molded integrally into the plastic body therewith, and electric leads extending from the ends of said electro-conductive strand means out of the plastic body, said frangible, electro-conductive strand means being of a strength which will break in the safe limits of stress imposed upon the plastic body are exceeded.
3. In combination, a hollow plastic body, flexible, body-reinforcing load-carrying strands embedded in and extending continuously through the plastic body and molded integrally therewith, flexible, frangible, electroconductive strand means forming a part of the load-carrying strands and extending parallel to and coextensive with the load-carrying strands and molded integrally into the plastic body therewith, and electric leads extending from the ends of said electro-conductive strand means out of 6 the plastic body, said frangible, electro-conductive strand means being of a strength which will break if the plastic body is cracked.
4. A reinforced plastic member including a hard, cured plastic body made rom a tape wound over itself to form the body, the tape havin a plurality of plastic-impregnated, flexible, load-carrying strands extending longitudinally of the tape and parallel to each other, and the tape having a single electro-conductive, plastic-impregnated, flexible but frangible strand means extending longitudinally of the tape and parallel to ti e load-carrying strands so as to be Wound entirely through the plastic body, and electric leads connected to the ends of the electro-conductive strand means and extending outside the body whereby the electrical continuity of the electro-conductive strand means can be tested at any time after the curing of the body to thereby provide a checx on the continuity of the body.
5. The combination defined in claim 3 wherein the electro-conductive strand means have an electrically nonconductive core means surrounded by an electro-conducti /e surface layer.
References Cited in the file of this patent UNITED STATES PATENTS 2,131,478 Mann Sept. 27, 1938 2,340,146 Ruge Jan. 25, 1944 2,449,883 De Forest Sept. 21, 1948 2,582,341 Levers et al Ian. 15, 1952 2,848,390 Whitehurst et a1 Aug. 19, 1958

Claims (1)

1. IN COMBINATION, A HOLLOW PLASTIC BODY, FLEXIBLE, BODY-REINFORCING LOAD-CARRYING STRANDS EMBEDDED IN AND EXTENDING HELICALLY AS A CONTINUOUS TAPE THROUGH THE PLASTIC BODY AND MOLDED INTEGRALLY THEREWITH, FLEXIBLE, FRANGIBLE, ELECTRO-CONDUCTIVE STRAND MEANS FORMING A PART OF THE TAPE AND EXTENDING PARALLEL TO AND COEXTENSIVE WITH THE LOAD-CARRYING STRANDS AND MOLDED INTEGRALLY INTO THE PLASTIC BODY THEREWITH, ELECTRIC LEADS EXTENDING FROM THE ENDS OF SAID ELECTRO-CONDUCTIVE STRAND MEANS OUT OF THE PLASTIC BODY, AND ELECTRICAL MEANS ADAPTED TO BE CONNECTED TO SAID LEADS FOR DETERMINING IF THE ELECTRO-CONDUCTIVE STRAND MEANS ARE UNBROKEN TO THEREBY DETERMINE THE SOUNDNESS OF THE PLASTIC BODY AFTER THE MAKING OR USE THEREOF, SAID FRANGIBLE, ELECTRO-CONDUCTIVE STRAND MEANS BEING OF A STRENGTH WHICH WILL BREAK IF THE SAFE LIMITS OF STRESS IMPOSED UPON THE PLASTIC BODY ARE EXCEEDED.
US855667A 1959-11-27 1959-11-27 Strain detection apparatus Expired - Lifetime US3080748A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US855667A US3080748A (en) 1959-11-27 1959-11-27 Strain detection apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US855667A US3080748A (en) 1959-11-27 1959-11-27 Strain detection apparatus

Publications (1)

Publication Number Publication Date
US3080748A true US3080748A (en) 1963-03-12

Family

ID=25321803

Family Applications (1)

Application Number Title Priority Date Filing Date
US855667A Expired - Lifetime US3080748A (en) 1959-11-27 1959-11-27 Strain detection apparatus

Country Status (1)

Country Link
US (1) US3080748A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3327271A (en) * 1964-01-23 1967-06-20 Daimler Benz Ag Strain gauge
US3603142A (en) * 1970-05-07 1971-09-07 Donald Saylak Method of detecting cracks and measuring strain in polymeric structures
US3635077A (en) * 1968-08-05 1972-01-18 Joseph Rauch Method for measuring deformation and gauge therefor
US3721898A (en) * 1968-12-04 1973-03-20 P Dragoumis Apparatus for detecting leakage from or rupture of pipes and other vessels containing fluid under pressure
US3779071A (en) * 1971-09-13 1973-12-18 Tracor Fatigue strain gauges
US3786679A (en) * 1972-04-12 1974-01-22 Battelle Memorial Institute Fatigue indication
US4111040A (en) * 1976-07-30 1978-09-05 Societe Nationale Elf Aquitaine (Production) Testing for corrosion of the internal wall of a metal chamber
US4185496A (en) * 1978-08-28 1980-01-29 Gould Inc. Thin film strain gage and process therefor
US4411159A (en) * 1980-07-12 1983-10-25 Rubery Owen Group Services Limited A fibre reinforced resin composite leaf spring for determining the magnitude of a load
US4498282A (en) * 1981-12-18 1985-02-12 Hoechst Aktiengesellschaft Wire rope having a durable marker
US4757719A (en) * 1986-05-15 1988-07-19 Spanset Inter Ag Round load lifting sling
US5581039A (en) * 1992-09-18 1996-12-03 Hitachi, Ltd. Ceramic body and method and apparatus for detecting change thereof
US6443016B1 (en) 2000-07-20 2002-09-03 Robert Sinelli Electric cable assembly with sacrificial conductors

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2131478A (en) * 1937-03-08 1938-09-27 Mann Hubert Galvanometer fiber or string
US2340146A (en) * 1941-10-02 1944-01-25 Arthur C Ruge Strain gauge
US2449883A (en) * 1945-01-08 1948-09-21 Baldwin Locomotive Works Fatigue indicator
US2582341A (en) * 1946-06-03 1952-01-15 Celanese Corp Electrical device
US2848390A (en) * 1953-11-10 1958-08-19 Owens Corning Fiberglass Corp Method and apparatus for applying metal to glass

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2131478A (en) * 1937-03-08 1938-09-27 Mann Hubert Galvanometer fiber or string
US2340146A (en) * 1941-10-02 1944-01-25 Arthur C Ruge Strain gauge
US2449883A (en) * 1945-01-08 1948-09-21 Baldwin Locomotive Works Fatigue indicator
US2582341A (en) * 1946-06-03 1952-01-15 Celanese Corp Electrical device
US2848390A (en) * 1953-11-10 1958-08-19 Owens Corning Fiberglass Corp Method and apparatus for applying metal to glass

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3327271A (en) * 1964-01-23 1967-06-20 Daimler Benz Ag Strain gauge
US3635077A (en) * 1968-08-05 1972-01-18 Joseph Rauch Method for measuring deformation and gauge therefor
US3721898A (en) * 1968-12-04 1973-03-20 P Dragoumis Apparatus for detecting leakage from or rupture of pipes and other vessels containing fluid under pressure
US3603142A (en) * 1970-05-07 1971-09-07 Donald Saylak Method of detecting cracks and measuring strain in polymeric structures
US3779071A (en) * 1971-09-13 1973-12-18 Tracor Fatigue strain gauges
US3786679A (en) * 1972-04-12 1974-01-22 Battelle Memorial Institute Fatigue indication
US4111040A (en) * 1976-07-30 1978-09-05 Societe Nationale Elf Aquitaine (Production) Testing for corrosion of the internal wall of a metal chamber
US4185496A (en) * 1978-08-28 1980-01-29 Gould Inc. Thin film strain gage and process therefor
US4411159A (en) * 1980-07-12 1983-10-25 Rubery Owen Group Services Limited A fibre reinforced resin composite leaf spring for determining the magnitude of a load
US4498282A (en) * 1981-12-18 1985-02-12 Hoechst Aktiengesellschaft Wire rope having a durable marker
US4757719A (en) * 1986-05-15 1988-07-19 Spanset Inter Ag Round load lifting sling
AU586102B2 (en) * 1986-05-15 1989-06-29 Spanset Inter Ag Round load lifting sling
US5581039A (en) * 1992-09-18 1996-12-03 Hitachi, Ltd. Ceramic body and method and apparatus for detecting change thereof
US6443016B1 (en) 2000-07-20 2002-09-03 Robert Sinelli Electric cable assembly with sacrificial conductors

Similar Documents

Publication Publication Date Title
US3080748A (en) Strain detection apparatus
US5528155A (en) Sensor for measuring material properties
KR101961408B1 (en) Monitoring method of CFRP damage
US4437138A (en) Force sensing means and method of producing such sensing means
US3067569A (en) Electrical conductors and methods of manufacture thereof
US3779071A (en) Fatigue strain gauges
US2669646A (en) Electrically conductive material
US3786679A (en) Fatigue indication
US20140368214A1 (en) Electric cable wear control system
KR102625041B1 (en) sensor device
CN111351597B (en) Fiber composite component, component system, aircraft, and use of lithiated carbon fibers
US20180011044A1 (en) Non-destructive wear monitoring system for synthetic ropes and textiles
US9329021B1 (en) System and methods for use in monitoring a structure
JPH0398889A (en) Manufacture or repair method for storage container and produced container
US2690984A (en) Electric cable jacket
US4236109A (en) Dielectric monitored composite assembly
KR101964880B1 (en) System and method for diagnosing crack propagation of CFRP structures
US4870365A (en) Measuring device, reinforcement rod, process for detecting mechanical defects in fiber composite building elements and application of the process
JPH07102621B2 (en) FRP and non-destructive inspection device for FRP
US4684293A (en) Cable for fastening structures and method of detecting damage to corrosion-preventive layer thereof
CN108181029A (en) The method of the multi-direction monitoring fibre reinforced composites strain of carbon nanometer paper sensor
KR102080411B1 (en) Fabric type smart grid sensor
US2449883A (en) Fatigue indicator
US3064221A (en) Force gages using strain-sensing wire elements and methods of making force gages
US2837620A (en) Strain gauges and load weighing cells